View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 53449U 26145.77719543 +.00000000 +00000-0 +76901-3 0 00005
2 53449 97.5456 275.9665 0000958 143.3217 216.8113 15.74392420 05
| Epoch (UTC): | 25 May 2026 18:39:09 |
| Eccentricity: | 0.0000958 |
| inclination: | 97.5456° |
| perigee height: | 346 km |
| apogee height: | 347 km |
| right ascension of ascending node: | 275.9665° |
| argument of perigee: | 143.3217° |
| revolutions per day: | 15.74392420 |
| mean anomaly at epoch: | 216.8113° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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